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Turbulence Models: Data from Other Experiments: Shock Wave / Turbulent Boundary Layer Flows at High Mach Numbers

Metadata Updated: August 22, 2025

Shock Wave / Turbulent Boundary Layer Flows at High Mach Numbers. This web page provides data from experiments that may be useful for the validation of turbulence models. This resource is expected to grow gradually over time. All data herein arepublicly available.

Access & Use Information

Public: This dataset is intended for public access and use. License: No license information was provided. If this work was prepared by an officer or employee of the United States government as part of that person's official duties it is considered a U.S. Government Work.

Downloads & Resources

References

http://turbmodels.larc.nasa.gov/index.html

Dates

Metadata Created Date November 12, 2020
Metadata Updated Date August 22, 2025
Data Update Frequency irregular

Metadata Source

Harvested from NASA Data.json

Additional Metadata

Resource Type Dataset
Metadata Created Date November 12, 2020
Metadata Updated Date August 22, 2025
Publisher National Aeronautics and Space Administration
Maintainer
Identifier NASA-850__3
Data First Published 2018-06-25
Data Last Modified 2025-07-17
Category Aerospace
Public Access Level public
Data Update Frequency irregular
Bureau Code 026:00
Metadata Context https://project-open-data.cio.gov/v1.1/schema/catalog.jsonld
Schema Version https://project-open-data.cio.gov/v1.1/schema
Catalog Describedby https://project-open-data.cio.gov/v1.1/schema/catalog.json
Harvest Object Id 93676b6c-3bcd-4f1d-9547-80aaad0e74fe
Harvest Source Id 58f92550-7a01-4f00-b1b2-8dc953bd598f
Harvest Source Title NASA Data.json
Homepage URL https://turbmodels.larc.nasa.gov/Other_exp_Data/cfdval2004_exp.html
Program Code 026:023
Related Documents http://turbmodels.larc.nasa.gov/index.html
Source Datajson Identifier True
Source Hash ff18c4d22d99126fd98cd7cdf9699602542c1533138fbc4ebb76fe3f0742a196
Source Schema Version 1.1

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